Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Dornier P.247/6 Fighter / Fighter-Bomber Design Study.
1 x Junkers Jumo 213T inverted-Vee liquid-cooled, turbocharged piston engine developing 2,000 horsepower driving four-bladed propeller unit in pusher arrangement.
Propulsion
519 mph
836 kph | 451 kts
Max Speed
36,745 ft
11,200 m | 7 miles
Service Ceiling
870 miles
1,400 km | 756 nm
Operational Range
1,800 ft/min
549 m/min
Rate-of-Climb